Ми-4 B.2 aircraft.cfg Просмотр ZIP-архива

Aircraft Aeroflot/Aircraft.cfg

[fltsim.0]
title=Mi-4 Aeroflot
sim=Mi-4 Aeroflot
model=
panel=
sound=
texture=
kb_checklists=
prop_anim_ratio=-0.43174
atc_id=CCCP-03586
atc_model=Mi-4 Aeroflot
ui_manufacturer=Mil
ui_type=Mi-4 Aeroflot
ui_variation=CCCP-03586
atc_heavy=0
atc_airline=Aeroflot
atc_flight_number=CCCP-03586

[General]
performance=Cruise Speed  80 kts\Maximum speed: 185 km/h (116 mph)\Powerplant: 1 Ч Shvetsov ASh-82V radial engine, 1,250 kW (1,675 hp)\Service ceiling: 5,500 m (18,040 ft)\nRate of Climb 600'per min\nFuel Capacity  Internal 185 U.S. gal\Range: 500 km (313 mi)\Empty weight: 5,100 kg (11,220 lb)\Max. takeoff weight: 7,550 kg (16,610 lb)\nSeating 2 Crew & 8-12 Passengers


[WEIGHT_AND_BALANCE]
max_gross_weight = 13600.000
empty_weight = 12755.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 6.709, 0.000, 0.000

max_number_of_stations = 12

station_load.0 =170.000000, 21.489000, -2.132000, -2.132000, Pilot
station_load.1 =170.000000, 21.489000, 2.135000, -2.132000, Co-Pilot
station_load.2 =170.000000, 20.177000, 0.000000, -2.130000, Engineer
station_load.3 =170.000000, 14.271000, -1.640000, -2.788000, Pass FrontLeft1
station_load.4 =170.000000, 14.271000, -3.280000, -2.788000, Pass FrontLeft2
station_load.5 =170.000000, 11.318000, -1.640000, -2.952000, Pass FRontLeft3
station_load.6 =170.000000, 11.318000, -3.280000, -2.952000, Pass FrontLeft4
station_load.7 =170.000000, 8.202000, -1.640000, -3.280000, Pass MiddleLeft
station_load.8 =170.000000, 8.202000, -3.280000, -3.280000, Pass MiddleLeft
station_load.9 =170.000000, 5.249000, -1.640000, -3.444000, Pass BackLeft1
station_load.10 =170.000000, 5.249000, -3.280000, -3.444000, Pass BackLeft2
station_load.11 =170.000000, 2.600000, -1.640000, -3.608000, Pass BackLeft3
station_load.12 =170.000000, 2.600000, -3.280000, -3.608000, Pass BackLeft4


;Moments of Inertia
empty_weight_roll_MOI= 50000.000
empty_weight_pitch_MOI= 50000.000
empty_weight_yaw_MOI= 106000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[flight_tuning]
rudder_effectiveness=0.05
aileron_effectiveness= 1.0
elevator_effectiveness=1.3

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot          = 4, 4 , 15.0
avionics           = 0, 5 , 15.0
pitot_heat         = 4, 2 , 15.0
additional_system  = 0, 2 , 15.0
marker_beacon      = 4, 2 , 10.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 24.0
starter2           = 0, 20, 24.0
starter3           = 0, 20, 24.0
light_nav          = 0, 5 , 10.0
light_beacon       = 4, 5 , 15.0
light_landing      = 4, 5 , 15.0
light_taxi         = 0, 5 , 15.0
light_strobe       = 0, 5 , 10.0
light_panel        = 0, 5 , 10.0
light_cabin        = 4, 5 , 10.0
light_logo         = 4, 5 , 10.0
light_recognition  = 4, 5 , 10.0
hydraulic_pump     = 0, 5 , 15.0
fuel_transfer_pump = 0, 5 , 15.0
max_battery_voltage = 38.0
generator_alternator_voltage = 208.0
max_generator_alternator_amps = 150.0

static_pitch = 3.4
static_cg_height = 6.5
max_number_of_points = 8
        //0  Class                        <0=none,1=wheel, 2=scrape, 3=skid>
        //1  Longitudinal Position        (feet)
        //2  Lateral Position             (feet)
        //3  Vertical Position            (feet)
        //4  Impact Damage Threshold      (Feet Per Minute)
        //5  Brake Map                    (0=None, 1=Left, 2=Right)
        //6  Wheel Radius                 (feet)
        //7  Steer Angle                  (degrees)
        //8  Static Compression           (feet)  (0 if rigid)
        //9  Max/Static Compression Ratio
        //10 Damping Ratio                (0=Undamped, 1=Critically Damped)
        //11 Extension Time               (seconds)
        //12 Retraction Time              (seconds)
        //13 Sound Type
        //14 Airspeed limit for retraction     (KIAS)
        //15 Airspeed that gear gets damage at (KIAS)

[contact_points]
point.0= 1.000, 18.864, 0.000, -11.750, 1574.000, 0.000, 0.984, 35.000, 0.760, 1.300, 0.750, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 4.757, -7.381, -10.440, 1600.000, 1.000, 1.476, 0.000, 0.800, 1.300, 0.850, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 4.757, 7.381, -10.440, 1600.000, 2.000, 1.476, 0.000, 0.800, 1.300, 0.850, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, 25.754, 0.000, -4.101, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=0.000000
static_cg_height=0.000000


[brakes]
parking_brake = 1      //Parking brake available
toe_brakes_scale = 0.3  //Brake scalar

[hydraulic_system]
normal_pressure=797.700
engine_map=1,0,0,0
electric_pumps=1

[Views]
eyepoint = 20.4, -2.15, -0.25

[exits]
number_of_exits=4
exit_rate.0=0.4                                                           
exit_rate.1=0.4      
exit_rate.2=0.4
exit_rate.3=0.4

[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 1
Com.2         = 1, 1
Nav.1         = 1, 1, 1
Nav.2         = 1, 1, 0
Adf.1         = 1 
Transponder.1 = 1
Marker.1      = 1

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
//NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque
elevator = 100,  180
aileron  = 200, 1000
rudder   = 200, 1000

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=2,0

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0


[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
landrotorwas=fx_rtr_lnd
waterrotorwash=fx_rtr_wt
touchdown=fx_tchdwn


[fuel]
Center1 = 6.889, 0.000, 2.296, 117.000, 0.000
fuel_type = 2                                //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors =3                    
electric_pump=1
External1= 8.366, -4.920, -4.757, 179.000, 0.000
External2= 9.350, 4.920, -4.757, 196.000, 0.000

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -2.75, 0.0, -1.8                     //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0                           //Fuel flow scalar
min_throttle_limit = 0.0                        //Minimum percent throttle.  Generally negative for turbine reverser
master_ignition_switch = 1                      //Master Ignition Switch
///==============================================
[piston_engine]
power_scalar = 0.93                           //Piston power scalar
cylinder_displacement= 190.71                   //Cubic inches per cylinder
compression_ratio= 6.7                          //Compression ratio
number_of_cylinders=14                          //Number of cylinders
max_rated_rpm= 4900                             //Max rated RPM
max_rated_hp= 1800                              //Max rated HP
fuel_metering_type= 1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.2             //Starter torque factor
turbocharged= 1                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 47                               //Max design manifold pressure, (inHg)
min_design_mp= 10                               //Min design manifold pressure, (inHg)
critical_altitude= 7000                        //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0                               //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0                   //Scalar on idle RPM friction

[Reference Speeds]
cruise_speed            = 129.0                 //Knots True (KTAS)
max_indicated_speed     = 134.0                   //Red line (KIAS)

[fuselage_aerodynamics]
drag_force_cf=0.000000
side_drag_force_cf=0.000000
pitch_damp_cf=1.500000
roll_damp_cf=1.000000
yaw_damp_cf=0.600000
yaw_stability_cf=2.500000

[MainRotor]
Position = 7.873, 0, 6.561
Radius = 34.931
max_disc_angle = 4.0
Number_of_blades = 4
weight_per_blade = 264.0
Weight_to_moi_factor = 42.0
inflow_wel_reference =43.0
inflow_vel_reference=0.000000
 
[SecondaryRotor]
TailRotor = 1
Position = -34.776, 2.378, 4.101
Radius = 6.397 

[autopilot]
autopilot_available= 0
flight_director_available= 0
attitude_indicator= 0
direction_indicator=0
default_pitch_mode=1
max_pitch=20.0
max_pitch_acceleration=5.0
default_vertical_speed=0.01
default_bank_mode=2
max_bank=30
max_bank_acceleration=1.5
autothrottle_available=0
pitch_takeoff_ga= 8.000
max_pitch_velocity_lo_alt= 5.000
max_pitch_velocity_hi_alt= 5.500
max_pitch_velocity_lo_alt_breakpoint= 20000.000
max_pitch_velocity_hi_alt_breakpoint= 28000.000
max_bank_velocity= 5.000
max_throttle_rate= 0.100
nav_proportional_control= 9.000
nav_integrator_control= 0.250
nav_derivative_control= 0.000
nav_integrator_boundary= 2.500
nav_derivative_boundary= 0.000
gs_proportional_control= 9.520
gs_integrator_control= 0.260
gs_derivative_control= 0.000
gs_integrator_boundary= 0.700
gs_derivative_boundary= 0.000
yaw_damper_gain= 5.000

[yaw_string]
yaw_string_available=1

[Helicopter]
reference_length=0.000000
reference_frontal_area=0.000000
reference_side_area=0.000000
side_aero_center=0.000000
right_trim_scalar=1.000000
correlator_available=1.000000
governed_pct_rpm_ref=1.000000
rotor_brake_scalar=1.000000
torque_scalar=1.000000
cyclic_roll_control_scalar=1.000000
cyclic_pitch_control_scalar=1.000000
pedal_control_scalar=1.000000
collective_on_rotor_torque_scalar=1.000000

47587-Ispravka.zip

Имя файла Дата Размер
Aircraft Aeroflot/ 23.12.2012 21:59
Aircraft Aeroflot/Aircraft.cfg 23.12.2012 21:58 11 KB
Aircraft FI/ 23.12.2012 21:57
Aircraft FI/Aircraft.cfg 23.12.2012 21:31 11 KB
Aircraft YU/ 23.12.2012 21:57
Aircraft YU/Aircraft.cfg 23.12.2012 21:56 11 KB
Read me.txt 23.12.2012 22:09 48 B
avsim_su.diz 24.12.2012 03:18 406 B
Итого: 33 KB
Исправления Aircraft.cfg файл, если кто-то после загрузке вертолета падения на хвост.
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